| Item type |
会議発表論文 / Conference Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
A Study on the Performance of the Fluidic Thrust Vector Control Utilizing Supersonic Coanda Effects |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
supersonic |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
thrust vector control |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
coanda effects |
| キーワード |
|
|
言語 |
en |
|
主題Scheme |
Other |
|
主題 |
calibration |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_5794 |
|
資源タイプ |
conference paper |
| 著者 |
Song, MyungJun
Yoon, SangHun
Chang, HongBeen
Cho, YongHo
Lee, Yeol
|
| 著者所属 |
|
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 著者所属 |
|
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 著者所属 |
|
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University : Agency for Defense Development |
| 著者所属 |
|
|
|
Microfriend Inc. |
| 著者所属 |
|
|
|
School of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 著者所属（英） |
|
|
|
en |
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 著者所属（英） |
|
|
|
en |
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 著者所属（英） |
|
|
|
en |
|
|
Graduate School, Department of Aerospace & Mechanical Engineering, Korea Aerospace University : Agency for Defense Development |
| 著者所属（英） |
|
|
|
en |
|
|
Microfriend Inc. |
| 著者所属（英） |
|
|
|
en |
|
|
School of Aerospace & Mechanical Engineering, Korea Aerospace University |
| 出版者 |
|
|
出版者 |
宇宙航空研究開発機構(JAXA) |
| 出版者（英） |
|
|
出版者 |
Japan Aerospace Exploration Agency (JAXA) |
| 書誌情報 |
宇宙航空研究開発機構特別資料
en : JAXA Special Publication
巻 JAXA-SP-13-001E,
p. 253-261,
発行日 2013-11-30
|
| 会議概要（会議名, 開催地, 会期, 主催者等）（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan |
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Co-flow fluidic thrust vector control is one of the efficient thrust-vectoring methods. The present technique controls the direction of a supersonic primary jet by utilizing coanda effects of the secondary jet exhausted at the nozzle exit. A multi-component force measurement system is developed to quantitatively evaluate the performance of the fluidic thrust control technique. Detailed calibration and data analysis have been performed to reduce measurement errors. It is found that the interaction error between load cells possibly introduced by misalignment of the test device is estimated to be less than 5%, and that the unwanted pressure errors associated with air supply tubes are negligible. Some preliminary thrust-vectoring test results and comparison with the results of flow visualization/numerical calculation are also provided. It is observed that the deflection angle the primary jet varies almost linearly with variation of the momentum ratio of the primary jet to the secondary coanda jet. |
| 内容記述 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
形態: カラー図版あり |
| 内容記述（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Physical characteristics: Original contains color illustrations |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
1349-113X |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA11984031 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: AA0062070020 |
| レポート番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
レポート番号: JAXA-SP-13-001E |
62070020.pdf (878.5 kB)
